CA3085054A1 - Systemes de commande d'aeronef - Google Patents
Systemes de commande d'aeronef Download PDFInfo
- Publication number
- CA3085054A1 CA3085054A1 CA3085054A CA3085054A CA3085054A1 CA 3085054 A1 CA3085054 A1 CA 3085054A1 CA 3085054 A CA3085054 A CA 3085054A CA 3085054 A CA3085054 A CA 3085054A CA 3085054 A1 CA3085054 A1 CA 3085054A1
- Authority
- CA
- Canada
- Prior art keywords
- control
- aircraft
- processing system
- inceptor
- input
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 claims description 23
- 230000001419 dependent effect Effects 0.000 claims description 22
- 230000007704 transition Effects 0.000 description 8
- 230000008859 change Effects 0.000 description 7
- 230000007423 decrease Effects 0.000 description 6
- 230000003247 decreasing effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/50—Steerable undercarriages; Shimmy-damping
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Mechanical Control Devices (AREA)
- Feedback Control In General (AREA)
- Radar Systems Or Details Thereof (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
L'invention concerne des systèmes de commande d'aéronef permettant d'utiliser des commandes d'entrée partagées. Un même organe de pilotage peut fournir des sorties permettant de commander des commandes d'aéronef au sol et des commandes d'aéronef dans l'air afin de réduire le nombre d'organes de pilotage requis. Dans un exemple, un manche latéral permet de commander à la fois le tangage et l'orientation du train avant de l'aéronef. Une technologie d'organe de pilotage active peut être utilisée pour fournir à l'opérateur une rétroaction sur l'état du système de commande.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1721529.4A GB2569601B (en) | 2017-12-21 | 2017-12-21 | Aircraft control systems |
GB1721529.4 | 2017-12-21 | ||
EP18151965.3A EP3511241A1 (fr) | 2018-01-16 | 2018-01-16 | Système de commande d'un aéronef |
EP18151965.3 | 2018-01-16 | ||
PCT/GB2018/053448 WO2019122807A1 (fr) | 2017-12-21 | 2018-11-29 | Systèmes de commande d'aéronef |
Publications (1)
Publication Number | Publication Date |
---|---|
CA3085054A1 true CA3085054A1 (fr) | 2019-06-27 |
Family
ID=64556943
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA3085054A Pending CA3085054A1 (fr) | 2017-12-21 | 2018-11-29 | Systemes de commande d'aeronef |
Country Status (9)
Country | Link |
---|---|
US (1) | US11174005B2 (fr) |
EP (1) | EP3728026B1 (fr) |
JP (1) | JP7005770B2 (fr) |
KR (1) | KR102650037B1 (fr) |
CN (1) | CN111556841B (fr) |
CA (1) | CA3085054A1 (fr) |
ES (1) | ES2949956T3 (fr) |
MA (1) | MA51273A (fr) |
WO (1) | WO2019122807A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2949956T3 (es) | 2017-12-21 | 2023-10-04 | Bae Systems Plc | Sistemas de control de aeronaves |
US20240228022A9 (en) * | 2022-10-19 | 2024-07-11 | Lockheed Martin Corporation | Mode-dependent tactile feedback profiles for an inceptor |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2621002A (en) * | 1948-11-23 | 1952-12-09 | Lockheed Aircraft Corp | Steerable landing gear for airplanes |
JPS5721059Y2 (fr) | 1976-08-06 | 1982-05-07 | ||
US4420808A (en) * | 1980-04-01 | 1983-12-13 | United Technologies Corporation | Multi-axis force stick, self-trimmed aircraft flight control system |
US5008825A (en) * | 1989-05-01 | 1991-04-16 | Nadkarni Arun A | Apparatus and methods for automatically maintaining aircraft track angle |
US5412299A (en) | 1993-12-21 | 1995-05-02 | Honeywell, Inc. | Variable servo loop compensation in an active hand controller |
US6671588B2 (en) | 2001-12-27 | 2003-12-30 | Toyota Jidosha Kabushiki Kaisha | System and method for controlling traveling direction of aircraft |
JP3817591B2 (ja) | 2002-05-14 | 2006-09-06 | 学校法人金沢工業大学 | 自動車 |
GB2444678B (en) | 2005-08-29 | 2010-09-22 | Borealis Tech Ltd | Nosewheel control apparatus |
GB2471213B (en) * | 2006-08-29 | 2011-05-11 | Borealis Tech Ltd | Nosewheel control apparatus |
US7840316B2 (en) | 2007-12-17 | 2010-11-23 | Honeywell International Inc. | Limited authority and full authority mode fly-by-wire flight control surface actuation control system |
US20090187292A1 (en) * | 2008-01-17 | 2009-07-23 | Mark Andrew Hreha | Integrated pitch, roll, and yaw inceptor |
EP2303610B1 (fr) * | 2008-07-28 | 2020-01-08 | Fleck Future Concepts GmbH | Véhicule routier, aquatique et aérien combiné |
FR2948629B1 (fr) * | 2009-07-28 | 2011-08-19 | Eurocopter France | Amortissement variable de restitution haptique pour chaine cinematique de changement d'attitude de vol d'un aeronef |
US9051045B2 (en) | 2010-07-28 | 2015-06-09 | Woodward Mpc, Inc. | Indirect drive active control column |
US8606437B2 (en) | 2011-11-28 | 2013-12-10 | Embraer S.A. | Flight control system mode and method providing aircraft speed control through the usage of momentary on-off control |
US20170297605A1 (en) * | 2014-10-08 | 2017-10-19 | Aeromobil, S.R.O. | A directional control system for a hybrid air and ground transportation vehicle |
GB2533179B (en) * | 2014-12-10 | 2020-08-26 | Airbus Operations Ltd | Control method and apparatus for an aircraft when taxiing |
ES2949956T3 (es) | 2017-12-21 | 2023-10-04 | Bae Systems Plc | Sistemas de control de aeronaves |
-
2018
- 2018-11-29 ES ES18811338T patent/ES2949956T3/es active Active
- 2018-11-29 CN CN201880082281.6A patent/CN111556841B/zh active Active
- 2018-11-29 EP EP18811338.5A patent/EP3728026B1/fr active Active
- 2018-11-29 WO PCT/GB2018/053448 patent/WO2019122807A1/fr unknown
- 2018-11-29 CA CA3085054A patent/CA3085054A1/fr active Pending
- 2018-11-29 KR KR1020207018166A patent/KR102650037B1/ko active IP Right Grant
- 2018-11-29 JP JP2020534188A patent/JP7005770B2/ja active Active
- 2018-11-29 MA MA051273A patent/MA51273A/fr unknown
- 2018-11-29 US US16/771,315 patent/US11174005B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20200339246A1 (en) | 2020-10-29 |
KR102650037B1 (ko) | 2024-03-20 |
US11174005B2 (en) | 2021-11-16 |
MA51273A (fr) | 2021-05-12 |
CN111556841A (zh) | 2020-08-18 |
JP7005770B2 (ja) | 2022-01-24 |
ES2949956T3 (es) | 2023-10-04 |
EP3728026A1 (fr) | 2020-10-28 |
KR20200095497A (ko) | 2020-08-10 |
CN111556841B (zh) | 2024-09-10 |
WO2019122807A1 (fr) | 2019-06-27 |
JP2021507846A (ja) | 2021-02-25 |
EP3728026B1 (fr) | 2023-05-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request |
Effective date: 20231128 |